CN105257604A - Turbine air compressor - Google Patents
Turbine air compressor Download PDFInfo
- Publication number
- CN105257604A CN105257604A CN201510736927.6A CN201510736927A CN105257604A CN 105257604 A CN105257604 A CN 105257604A CN 201510736927 A CN201510736927 A CN 201510736927A CN 105257604 A CN105257604 A CN 105257604A
- Authority
- CN
- China
- Prior art keywords
- air
- turbine
- air compressor
- compressor
- suction port
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000000446 fuel Substances 0.000 claims abstract description 19
- 238000005516 engineering process Methods 0.000 claims description 4
- 241000168254 Siro Species 0.000 claims description 3
- 238000009987 spinning Methods 0.000 claims description 3
- 230000008901 benefit Effects 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000000192 social effect Effects 0.000 abstract description 2
- 238000001914 filtration Methods 0.000 abstract 3
- 239000003381 stabilizer Substances 0.000 abstract 3
- 230000006835 compression Effects 0.000 abstract 2
- 238000007906 compression Methods 0.000 abstract 2
- 239000007789 gas Substances 0.000 description 10
- 238000005457 optimization Methods 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000000314 lubricant Substances 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 230000001737 promoting effect Effects 0.000 description 2
- 206010014405 Electrocution Diseases 0.000 description 1
- 206010053615 Thermal burn Diseases 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 238000004887 air purification Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000000855 fermentation Methods 0.000 description 1
- 230000004151 fermentation Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 230000029058 respiratory gaseous exchange Effects 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses a turbine air compressor. The turbine air compressor comprises main shafts, air inlets, filtering devices, an air compression machine, a fuel pipe, a fuel chamber, a turbine, an exhaust opening, stabilizer blades and a base plate; the four stabilizer blades are arranged on the surface of the base plate, and the air inlets are formed in the top ends of the stabilizer blades; the main shafts are installed inside the air inlets, and the filtering devices are arranged inside the air inlets; and the filtering devices are tightly connected with the air compression machine. Compared with the prior art, the novel turbine air compressor has the beneficial effects that air can be purified, so that air entering the turbine air compressor is clean, the working efficiency of the air compressor is improved, the turbine air compressor is compact in structure, convenient to carry, long in service life, low in manufacturing cost and suitable for application and popularization, and has the good social effect and the good economic benefit.
Description
Technical field
The present invention relates to a kind of buckle, especially a kind of turbocompressor.
Background technique
Many by the energy through using, each energy has its particular range, and applicability respectively has pluses and minuses, undeniable, and electric power is the energy of the most universal also most convenience in all energy; Secondly, pressurized air can say it is one of universal energy being only second to electric power, although compressed-air actuated use is goed deep in general family not yet as electric power, but industry, mining industry, engineering, hospitality industry even agricultural have purposes increasingly widely, pollution-free or low stain, in the epoch that environmental consciousness is surging, pressurized air is taken from air and returns in air, do not need recycling and pollution can not be manufactured completely, in process of production, pressurized air directly can contact with product most absolutely and transmits power and can not injure product.Without pyrophorisity, be not easy to cause public accident, except pressurized container needs to arrange according to the rules and make regular check on, do not cause the misgivings of public hazards, electrocution completely.Temperature is not high, be not easy to cause burn, the great bodily injury such as scald.Nitrogen, oxygen, hydrogen nitrogen or rare gas can be produced to supply specific use with stripping technique.There is provided non-power applications, the special-purposes such as such as personnel's breathing, water treatment, fermentation and chemical reaction.
Summary of the invention
The object of the present invention is to provide a kind of turbocompressor, to solve the problem proposed in above-mentioned background technology.
The object of the invention is to be achieved by following technical proposals: a kind of turbocompressor, comprise main shaft, suction port, filtrating equipment, gas compressor, fuel pipe, fuel chambers, turbine, relief opening, leg and base plate, described backplate surface is provided with four legs and described leg top is provided with suction port; Described suction port inside is provided with main shaft and described suction port inside is provided with filtrating equipment; Described filtrating equipment and gas compressor compact siro spinning technology.
Further, described filtrating equipment side is provided with gas compressor.
Further, described gas compressor one end is provided with fuel pipe.
Further, described fuel pipe side is provided with the fuel chambers of frustoconic shape structure.
Further, described turbine side is provided with the turbine being positioned at leg top.
Further, described turbine side is provided with relief opening.
Compared with prior art, the invention has the beneficial effects as follows this novel a kind of turbocompressor, can by air purification, make the air cleaning entering its inside, add the working efficiency of compressor, compact structure, be easy to carry, working life is of a specified duration, manufacturing price is cheap, be applicable to promoting the use of, have good social effect and economic benefit.
Accompanying drawing explanation
Fig. 1 is positive effect figure of the present invention;
In figure: 1, main shaft, 2, suction port, 3, filtrating equipment, 4, gas compressor, 5, fuel pipe, 6, fuel chambers, 7, turbine, 8, relief opening; 9, leg, 10, base plate.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention; technological scheme in the embodiment of the present invention is clearly and completely described; obviously; described embodiment is only the present invention's part embodiment; instead of whole embodiments; based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.
As shown in Figure 1, the invention discloses a kind of turbocompressor, comprise main shaft 1, suction port 2, filtrating equipment 3, gas compressor 4, fuel pipe 5, fuel chambers 6, turbine 7, relief opening 8, leg 9 and base plate 10, it is characterized in that, described base plate 10 surface is provided with four legs 9 and described leg 9 top is provided with suction port 2; Described suction port 2 inside is provided with main shaft 1 and described suction port 2 inside is provided with filtrating equipment 3; Described filtrating equipment 3 and gas compressor 4 compact siro spinning technology.
As a kind of technical optimization bill of the present invention, described filtrating equipment 3 side is provided with gas compressor 4.
As a kind of technical optimization bill of the present invention, described gas compressor 4 one end is provided with fuel pipe 5.
As a kind of technical optimization bill of the present invention, described fuel pipe 5 side is provided with the fuel chambers 6 of frustoconic shape structure.
As a kind of technical optimization bill of the present invention, described turbine 7 side is provided with the turbine 7 being positioned at leg 9 top.
As a kind of technical optimization bill of the present invention, described turbine 7 side is provided with relief opening 8.
The present invention in use, air compressor is in compressed-air actuated process, whether classify with mixing of lubricant oil with air, can divide into oily formula and oil-free compressor two kinds, lubricant oil all has lubrication and the effect cooled, for there being oily formula air compressor to any machinery, lubricant oil also has the airtight volumetric efficiency being used for promoting air compressor, therefore, from energy-conservation viewpoint, there is the energy efficiency of oily formula air compressor definitely can higher than oil-free compressor.Widely, it is to meeting above demand for the covering scope of air inlet, exhaust pressure.The covering scope of air quantity is also quite extensive, although in the application of Wind Volume oneself gradually replace by the air compressor of other type and withdraw from the market, in the using scope of little air quantity, still there is suitable advantage.In the application of little air quantity, high pressure, reciprocating air compressor can use as pressure-increasing machine.
To those skilled in the art, obviously the invention is not restricted to the details of above-mentioned one exemplary embodiment, and when not deviating from spirit of the present invention or essential characteristic, the present invention can be realized in other specific forms.Therefore, no matter from which point, all should embodiment be regarded as exemplary, and be nonrestrictive, scope of the present invention is limited by claims instead of above-mentioned explanation, and all changes be therefore intended in the implication of the equivalency by dropping on claim and scope are included in the present invention.Any reference character in claim should be considered as the claim involved by limiting.
In addition, be to be understood that, although this specification is described according to mode of execution, but not each mode of execution only comprises an independently technological scheme, this narrating mode of specification is only for clarity sake, those skilled in the art should by specification integrally, and the technological scheme in each embodiment also through appropriately combined, can form other mode of executions that it will be appreciated by those skilled in the art that.
Claims (6)
1. a turbocompressor, comprise main shaft (1), suction port (2), filtrating equipment (3), gas compressor (4), fuel pipe (5), fuel chambers (6), turbine (7), relief opening (8), leg (9) and base plate (10), it is characterized in that, described base plate (10) surface is provided with four legs (9) and described leg (9) top is provided with suction port (2); Described suction port (2) inside is provided with main shaft (1) and described suction port (2) inside is provided with filtrating equipment (3); Described filtrating equipment (3) and gas compressor (4) compact siro spinning technology.
2. a kind of turbocompressor according to claim 1, is characterized in that, described filtrating equipment (3) side is provided with gas compressor (4).
3. a kind of turbocompressor according to claim 1, is characterized in that, described gas compressor (4) one end is provided with fuel pipe (5).
4. a kind of turbocompressor according to claim 1, is characterized in that, described fuel pipe (5) side is provided with the fuel chambers (6) of frustoconic shape structure.
5. a kind of turbocompressor according to claim 1, is characterized in that, described turbine (7) side is provided with the turbine (7) being positioned at leg (9) top.
6. a kind of turbocompressor according to claim 1, is characterized in that, described turbine (7) side is provided with relief opening (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510736927.6A CN105257604A (en) | 2015-11-03 | 2015-11-03 | Turbine air compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510736927.6A CN105257604A (en) | 2015-11-03 | 2015-11-03 | Turbine air compressor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105257604A true CN105257604A (en) | 2016-01-20 |
Family
ID=55097470
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510736927.6A Pending CN105257604A (en) | 2015-11-03 | 2015-11-03 | Turbine air compressor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105257604A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105781944A (en) * | 2016-03-10 | 2016-07-20 | 蚌埠市荣强压缩机制造有限公司 | Filtering device of natural gas compressor unit pipeline |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101329077A (en) * | 2008-07-29 | 2008-12-24 | 上海泰硕商务信息咨询有限公司 | Internal-burning type oil smoke discharging method and device |
| CN101529163A (en) * | 2006-09-14 | 2009-09-09 | 索拉透平公司 | Gas turbine fuel injector with a removable pilot assembly |
-
2015
- 2015-11-03 CN CN201510736927.6A patent/CN105257604A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101529163A (en) * | 2006-09-14 | 2009-09-09 | 索拉透平公司 | Gas turbine fuel injector with a removable pilot assembly |
| CN101329077A (en) * | 2008-07-29 | 2008-12-24 | 上海泰硕商务信息咨询有限公司 | Internal-burning type oil smoke discharging method and device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105781944A (en) * | 2016-03-10 | 2016-07-20 | 蚌埠市荣强压缩机制造有限公司 | Filtering device of natural gas compressor unit pipeline |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160120 |
|
| WD01 | Invention patent application deemed withdrawn after publication |